Geographic area monitoring systems and methods through interchanging tool systems between unmanned vehicles

ABSTRACT

In some embodiments, unmanned task systems are provided that comprise multiple unmanned vehicles each comprising: a control circuit; a motor; and a propulsion system coupled with the motor and configured to enable the respective unmanned vehicles to move themselves; and wherein a first control circuit of a first unmanned vehicle of the multiple unmanned vehicles is configured to identify a second unmanned vehicle carrying a first tool system configured to perform a first function, cause a notification to be communicated to the second unmanned vehicle directing the second unmanned vehicle to transfer the first tool system to the first unmanned vehicle, and direct a first propulsion system of the first unmanned vehicle to couple with the first tool system being transferred from the second unmanned vehicle.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a continuation of U.S. application Ser. No.15/699,942, filed Sep. 8, 2017, which claims the benefit of U.S.Provisional Application No. 62/385,390, filed Sep. 9, 2016, which isincorporated herein by reference in its entirety.

TECHNICAL FIELD

This invention relates generally to monitoring geographic areas.

BACKGROUND

Geographic areas can have numerous different uses. Often, activitiesand/or conditions regarding the areas may be determined and monitored.Obtaining the information can be time consuming and costly.

BRIEF DESCRIPTION OF THE DRAWINGS

Disclosed herein are embodiments of systems, apparatuses and methods tomonitor areas with unmanned vehicles. This description includesdrawings, wherein:

FIG. 1 illustrates a simplified block diagram of an exemplary unmannedvehicle task coordination system, in accordance with some embodiments.

FIG. 2 illustrates a simplified block diagram, cross-sectional view ofan exemplary UAV, in accordance with some embodiments.

FIG. 3 illustrates a simplified block diagram of an exemplary toolsystem, in accordance with some embodiments.

FIG. 4 illustrates a simplified block diagram, cross-sectional view ofan exemplary UAV and an exemplary tool system, in accordance with someembodiments.

FIG. 5 illustrates a simplified block diagram, cross-sectional view ofan exemplary UAV, in accordance with some embodiments.

FIG. 6 illustrates an exemplary system for use in implementing methods,techniques, devices, apparatuses, systems, servers, and sources enablingunmanned vehicle task coordination, in accordance with some embodiments.

FIG. 7 illustrates a simplified flow diagram of an exemplary process ofperforming tasks through multiple UAVs, in accordance with someembodiments.

FIG. 8 illustrates a simplified flow diagram of an exemplary process ofperforming tasks through multiple UAVs, in accordance with someembodiments.

FIG. 9 illustrates a simplified flow diagram of an exemplary process ofmanaging tasks through the cooperative operation of multiple UAVs, inaccordance with some embodiments.

FIG. 10 illustrates a simplified flow diagram of an exemplary process ofperforming distributed computational processing across multiple UAVs, inaccordance with some embodiments.

FIG. 11 illustrates a simplified flow diagram of an exemplary process ofenabling the handoff of tool systems between UAVs, in accordance withsome embodiments.

FIG. 12 illustrates a simplified flow diagram of an exemplary process ofbalancing power while managing UAVs in the performance of tasks, inaccordance with some embodiments.

Elements in the figures are illustrated for simplicity and clarity andhave not necessarily been drawn to scale. For example, the dimensionsand/or relative positioning of some of the elements in the figures maybe exaggerated relative to other elements to help to improveunderstanding of various embodiments of the present invention. Also,common but well-understood elements that are useful or necessary in acommercially feasible embodiment are often not depicted in order tofacilitate a less obstructed view of these various embodiments of thepresent invention. Certain actions and/or steps may be described ordepicted in a particular order of occurrence while those skilled in theart will understand that such specificity with respect to sequence isnot actually required. The terms and expressions used herein have theordinary technical meaning as is accorded to such terms and expressionsby persons skilled in the technical field as set forth above exceptwhere different specific meanings have otherwise been set forth herein.

DETAILED DESCRIPTION

The following description is not to be taken in a limiting sense, but ismade merely for the purpose of describing the general principles ofexemplary embodiments. Reference throughout this specification to “oneembodiment,” “an embodiment,” “some embodiments”, “an implementation”,“some implementations”, “some applications”, or similar language meansthat a particular feature, structure, or characteristic described inconnection with the embodiment is included in at least one embodiment ofthe present invention. Thus, appearances of the phrases “in oneembodiment,” “in an embodiment,” “in some embodiments”, “in someimplementations”, and similar language throughout this specificationmay, but do not necessarily, all refer to the same embodiment.

Generally speaking, pursuant to various embodiments, systems,apparatuses and methods are provided to utilize unmanned aerial vehicles(UAVs) to perform various tasks at one or more geographic areas. In someembodiments, the UAVs can include a UAV control circuit cooperated withone or more motors and a propulsion system coupled with the motor andconfigured to enable the UAV to move itself. The UAV control circuit canidentify a task to be performed by the UAV and to identify a set of oneor more tool systems to be used to perform the task. The UAV controlcircuit is further configured to control the operation of the UAV indirecting the UAV to interchangeably and temporarily couple with atleast one of the set of tool systems in order to initiate the task theUAV determined is to be performed. In some embodiments, a UAV furtherincludes a universal coupler that includes a coupling system, and insome implementations includes a communication bus communicativelycoupled with the UAV control circuit. The universal coupler enables theinterchangeable coupling and decoupling of one or more of multipledifferent tool systems each having different functions to be put intouse while and/or after carried by the UAV. The coupling system of theuniversal coupler secures at least one tool system with the UAV, and insome instances enables a communication connection between thecommunication bus and the tool system. The tool systems each areconfigured to perform at least one function. The different functionscapable of being performed by the different tool systems are numerous.For example, some of the tool systems include a package securing toolsystem configured to retain and enable transport of a package whilebeing delivered, a sensor tool system configured to sense a conditionand communicate sensor data of the sensed condition to the UAV controlcircuit over the communication bus, camera tool systems configured tocapture images and/or video, lighting tool systems configured to emitlight at an intended wavelength, chemical dispensing systems configuredto dispense a chemical at one or more locations and/or over at least aportion of a geographic area, and other such tool systems.

FIG. 1 illustrates a simplified block diagram of an exemplary unmannedvehicle task coordination system 100, in accordance with someembodiments. The system includes one or more central control systems 102and multiple unmanned aerial vehicles (UAV) 104. The system mayadditionally or alternatively include multiple unmanned ground vehicles(UGV), marine or aquatic unmanned vehicles (subsurface and/or abovesurface), amphibious unmanned vehicles, other such unmanned vehicles, orcombination of two or more of such types of unmanned vehicles. In aneffort to simplify the description, the below is described withreference to UAVs; however, some or all of the operations, functions,and/or features of the system can be implemented through UGVs, marineunmanned vehicles, amphibious vehicles, UAVs, other such unmannedvehicles, or combination of two or more of such unmanned vehicles. Atleast some of the UAVs are configured to releasably cooperate with oneor more tool systems 106 that each can be utilized to perform one ormore tasks and/or provide functionality to the UAVs. The central controlsystem 102 is configured to communicate, via wired and/or wirelesscommunication, with the UAVs 104 through one or more computer and/orcommunication networks 108. Further, in some embodiments, the centralcontrol system and/or the UAVs may have access to one or more databases112 of information, programming, code, data and/or other such relevantinformation through direct coupling and/or via the one or more networks108.

In some embodiments, the task coordination system 100 may include one ormore mounting stations 114 and/or docking stations. At least some of themounting stations are configured to support one or more tool systems 106in a predefined orientation and/or configuration to enable the UAVs totemporarily cooperate with and remove one or more tool systems. Further,the mounting stations may be configured to allow UAVs to position one ormore tool systems with the mounting station and disengage from one ormore tool systems. In some implementations, a UAV may communicate withthe mounting station providing information about a tool system to beretrieved, and the mounting station can take steps to prepare the toolsystem (e.g., direct power to the tool system to recharge the internalpower source, move the tool system into a position to be cooperated withthe UAV, confirm the tool system is in operating conditions (e.g., basedon previous input information, applying testing, etc.), and/or othersuch actions).

The task coordination system 100 may, in some embodiments, include oneor more sensors and/or sensor systems 116 that can communicationinformation to the UAVs and/or the central control system. Further, oneor more of the sensor systems may be incorporated into tool systems tobe carried by, implemented by and/or utilized by a UAV. The sensorsystems may communicate directly with a UAV and/or communicate via wiredand/or wireless communication over one or more of the computer and/orcommunication networks 108. In some embodiments, the system 100 mayinclude one or more remote scheduling and/or service requestors 122configured to provide scheduling of tasks and/or submit requests thatone or more tasks be performed. Typically, the scheduling and/orrequests are communicated to the central control system 102; however, insome instances, the scheduling and/or requests may be directed to one ormore of the UAVs 104.

FIG. 2 illustrates a simplified block diagram, cross-sectional view ofan exemplary UAV 104, in accordance with some embodiments. FIG. 3illustrates a simplified block diagram of an exemplary tool system 106,in accordance with some embodiments. Referring to FIGS. 1-3, the UAV 104includes one or more UAV control circuits 202, one or more lift motors204, one or more propulsion systems 206 and a substructural support 208,body, frame, housing and/or other support structure to support at leastthe plurality of lift motors, propulsion systems and other components ofthe UAV. In some embodiments, the substructural support includes ahousing that encloses some or all of a series of components. In otherembodiments, the substructural support comprises a simple framing thatsupports the components for operation. Further, the substructuralsupport may be configured, in some applications, to enable components tobe readily added or removed and/or to enable parts of the substructuralsupport to be removed or added.

A UAV control circuit 202 is secured with the substructural support andcouples with the lift motors and in part is configured to control theoperation of the lift motors in controlling lift and movement of theUAV. Each propulsion system 206 may include one or more propellers,gearing and the like that cooperate with one or more of the lift motors.Similarly, in some embodiments, with some UAVs and/or UGVs, thepropulsion system may include one or more wheels, axels, gearing,transmissions and/or other such components to enable movement along theground or other surface. In some instances, the UAV control circuitcontrols the rotations per minute of the propellers (or wheels) toachieve the desired lift and/or propulsion for the UAV.

Typically, the UAV further includes a rechargeable electrical powersource 212 coupled with the UAV control circuit and the plurality oflift motors supplying electrical power to the UAV control circuit andthe plurality of lift motors. The rechargeable power source can includeone or more rechargeable batteries, capacitors, other such electricalpower storage devices, or combination of two or more of such powersources. Some embodiments further include one or more sets ofphotovoltaic cells and/or solar panels to supply electrical power to therechargeable power source. Additionally or alternatively, the UAV mayinclude a power coupler to enable the UAV to temporarily electricallycouple with an external power source to recharge the rechargeable powersource.

Further, many if not all of the UAVs 104 of the task coordination system100 further include a universal coupler 214 configured tointerchangeably couple and decouple one or more of the multipledifferent tool systems 106 with the UAV. Again, different tool systemsmay be configured to perform different functions and/or be used whileimplementing different tasks. By enabling the interchanging of toolsystems, a single UAV can be utilized to implement multiple differenttasks.

In some embodiments, the universal coupler includes one or more couplingsystems 216 configured to secure at least one of tool systems with theUAV. At least some of the tool systems 106 similarly include one or morecoupling systems 316 that are configured to securely couple with anddecouple from at least one coupling system 216 of a universal coupler214. Further, in some embodiments, the universal coupler includes one ormore communication buses 220, lines, or the like that communicativelycoupled with the UAV control circuit 202, and can furthercommunicatively couple with at least one or more communicationinterfaces 222, ports, contacts, and/or other such communicationconnections, which are configured to communicatively coupled with one ormore similar or mating communication interfaces 322, ports, contacts,and/or other such communication connections of a cooperated tool system106. Similarly, the tool system includes a communication line, bus orthe like establishing communication between at least the tool systemcontrol circuit 302 and the one or more communication interfaces 322.

The coupling systems 216, 316 and/or the universal coupler 214 caninclude one or more slots, latching systems, retractable pins, pinapertures to receive retractable pins, biased levers, notches, guiderails, slots or grooves (e.g., to receive guide rails), rotational barswith corresponding motors and corresponding cavities to receive andallow the bars to rotate, one or more sets of magnets, one or more setsof electromagnets, flexible latches and corresponding ledges or otherengaging surfaces, threaded bolts and corresponding threaded apertures,clips, other such structures, or combination of two or more of suchsecuring structures to temporarily secure at least one tool system 106with the universal coupler. One or more actuators, motors or the likemay be included with the coupling system and controlled by the UAVcontrol circuit to cause the coupling system to engage, lock orotherwise secure a tool system with the UAV, and similarly cause thecoupling system to unlock, disengage or otherwise release the toolsystem to allow the UAV to separate from the tool system. While secured,the communication interface 222 is configured to establish acommunication connection between the communication bus 220 and one ormore tool systems 106.

Still referring to FIGS. 1-3, the tool systems 106 include one or morefunctional systems 310 that are configured to provide the functionalityto the tool system to enable the tool system to perform one or morefunctions and/or tasks. In some implementations, for example, afunctional system 310 may include: one or more cameras to enable a toolsystem to capture images and/or video content; one or more sensors toenable the tool system to obtain sensor data that can be communicated tothe UAV control circuit and/or a remote processing system (e.g., thecentral control system 102, third party processing system and/orservice, etc.); one or more package securing tool systems configured toretain and enable transport of one or more items (e.g., packages whilebeing delivered, moved or the like); one or more lighting systems toemit light over a desired area; one or more chemical dispensing systems;one or more communication systems to enable the tool system to provide acommunication hub, repeater, network access point, and/or other suchcommunication functionality; one or more audio systems to capture audiocontent and/or playback audio content; one or more electrical chargeemitters; one or more radar systems; one or more motion detectors; oneor more sonar systems; one or more laser systems; one or more distancemeasurement systems; one or more light detectors; one or more humiditysensors; one or more chemical detector systems; one or more soil testingsystems; one or more infrared camera systems; one or more insect zappingsystems; one or more produce evaluation systems (e.g., light emittingsystem and corresponding detect to evaluate color, density, etc.); oneor more ground penetrating radar systems; other such functional systems;or combination of two or more of such functional systems. The sensorscan be substantially any relevant sensor and may be activated while theUAV is in flight, while the UAV is hovering, while the UAV is in astationary position (e.g., on the ground, on or in a mounting station,on or in a staging area, etc.), and/or when a tool system is disengagedfrom the UAV (e.g., UAV may be tasks to transport and position a sensortool system to within a threshold distance of a predefined location). Byenabling the coupling and decoupling of the multiple different toolsystems, individual UAVs can be utilized to implement differentfunctions and/or tasks. Similarly, the UAVs do not have to carry excessfunctionality that may add weight and/or cause a drain on power, whichcan result in reduced operating times, less range of travel, reducedpotential functionality, and the like. Instead, the UAVs can disengagefrom a tool system that does not include a functional system intended tobe utilized by the UAV and/or that a UAV is not transporting.

In some embodiments, the tool system includes one or more tool systemcontrol circuits 302 configured to provide at least some control overthe one or more functional systems 310 and/or to obtain information fromone or more functional systems. Some embodiments enable the UAV controlcircuit 202 to provide at least some control over the functional systems310 directly or through the tool system control circuit 302, while inother embodiments the tool system may not include a tool system controlcircuit and the UAV control circuit may directly control the one or morefunctional systems through the communication interfaces 222, 322. Inother embodiments, the tool control system can control at least thefunctional systems independent of the UAV. Further, the UAV controlcircuit may provide information to the tool system control circuitand/or the functional system, and/or relay information to the toolsystem control circuit and/or the functional system. In someembodiments, the tool system further includes computer and/or processormemory configured to store data, such as sensor information, operatingparameters, operating instructions, and/or other such information thatmay be accessed by the tool system control circuit 302 and/or the UAVcontrol circuit 202 of the UAV cooperated with the tool system. Further,the memory of the tool system may be utilized to store information sothat the UAV does not have to store the information. For example, sensordata captured by one or more sensor functional systems can be stored onthe tool system instead of storing the information in computer and/orprocessor readable memory of the UAV.

In some applications, the UAV supplies power to the tool system tooperate the one or more functional systems 310. Some tool systems 106may include one or more power sources 312 that provide power to the toolsystem control circuit 302 and one or more functional systems 310.Typically, the tool system power source 312 is a rechargeable powersource enabling repeated recharging and discharging of the power source.The tool system can be configured to couple with a power line or othercoupling of a mounting station 114 or other source to recharge the toolsystem power source. The power stored in the tool system power source312 allows the tool system to operate while limiting or preventingdrawing power from the UAV, which can allow for greater operatingdurations of the UAV. Additionally or alternatively, the UAV may supplypower to recharge the tool system power source. Similarly, the UAV mayin some instances draw power from the tool system power source to extendoperation of the UAV. In some embodiments, the UAV may not include apower source or have a limited power source 212, and draw power from theone or more tool systems cooperated with the UAV.

FIG. 4 illustrates a simplified block diagram, cross-sectional view ofan exemplary UAV 104 and an exemplary tool system 106, in accordancewith some embodiments. Referring to FIGS. 1-4, in some embodiments, theuniversal coupler 214 includes one or more alignment assemblies and/orsystems that are configured to aid in aligning the universal couplerwith a coupler system of a tool system. Similarly, the tool system mayadditionally or alternatively include one or more alignment assembliesand/or systems, which in some instances are configured to cooperate withalignment assemblies and/or systems of the universal coupler. Thealignment systems can include one or more assemblies, structures and/orcomponents to aid in cooperating and/or aligning the UAV with the toolsystem and/or the tool system with the UAV. In some embodiments, forexample, an alignment system of the universal coupler may include atapered and/or generally cone shaped cavity 402, while the alignmentsystem of the tool system may include a corresponding tapered orgenerally cone shaped protrusion 404. The universal coupler 214, in someembodiments, may additionally or alternatively include one or morealignment structures 414 configured to engage and cooperate with one ormore alignment structures 416 of a tool system as at least one of thetool system and the UAV is moved to cause the secure coupling betweenthe UAV and the tool system. For example, one more protrusions, rails,guides, or the like may be configured to engage one or morecorresponding recesses, slots, or the like. In some instances, thealignment structure 414 may include an extension and the alignmentstructure 416 may include a stop element with the extension configuredto engage the stop element formed in a mating surface of the toolsystem.

In some embodiments, the UAV and/or the universal coupler include one ormore sets of at least one permanent magnet 406 positioned to interactwith a surface of the tool system and/or one or more sets of at leastone permanent magnet 408 of a tool system 106 being cooperated with theuniversal coupler 214. In some applications, the sets of magnets can atleast assist in aligning the tool system with the universal coupler, andin some instances aid in maintaining a position of the tool systemrelative to the universal coupler. Additionally or alternatively, insome embodiments, the universal coupler and/or tool system includes oneor more sets of at least one electromagnet 410, which in someapplications may be positioned relative to at least one of the permanentmagnets 406, 408. The UAV control circuit can be configured to activatethe set of electromagnets 410 to aid in disengaging from the toolsystem. In some instances, the electromagnets can be activated to inpart overcome a magnetic force relative to one or more sets of permanentmagnets to cause a decoupling of the tool system from the UAV.

FIG. 5 illustrates a simplified block diagram, cross-sectional view ofan exemplary UAV 104, in accordance with some embodiments. The UAVand/or the universal coupler 214 includes one or more gripping systems502. In some embodiments, the gripping system comprises one or more clawelements 504, contracting elements and/or other such elements configuredto expand and retract as controlled by the UAV control circuit to gripone or more tool systems or other items (e.g., packages, tools, etc.).Further, in some applications the gripping system may include or besecured with an extending and retracting system 506 that can extend andretract the gripping system or at least the claw elements away from andtoward the substructural support 208. The gripping system can, forexample, be extended to cooperate with a grip feature of a tool system,and be retracted to secure and couple the tool system with the UAV. Theextending and retracting system 506 can include a crane system (e.g.,with one or more crane motors, spools and cable or rope that can belowered and retracted through the rotation of the spool by the cranemotor), piston and cooperated hydraulics or other compressed gas orfluid, and/or other such systems. For example, a tool system may includea crane system and package delivery system described in U.S. PatentApplication No. 62/222,572, filed Sep. 23, 2015, entitled Systems andMethods of Delivering Products with Unmanned Delivery Aircraft, which isincorporated herein by reference in its entirety. As another example,the tool system may include and/or cooperate with a package cooperationand release system described in U.S. Patent Application No. 62/222,575,filed Sep. 23, 2015, entitled Package Release System for Use in DeliveryPackages, and Methods of Delivering Packages, which is incorporatedherein by reference in its entirety.

In some implementations, the tool system may rotate as the extending andretracting system retracts a gripped tool system. As such, in someembodiments the universal coupler may comprises one or more structuresand/or components to limit or stop the rotation. For example, someembodiments include one or more extensions 512 that is configured toengage a stop element formed in a mating surface of the tool system. Theextension may further at least assist in aligning and inhibitingrotation of the tool system while the gripping system is retracted atleast a threshold distance from the universal coupler. For example, theextension may be a spring biased rod, a flexible rod or other suchextension that engages a ridge, recess, groove or other structure formedin a surface of the tool system. In other instances, for example, thestop element may be a recess or groove in the universal coupler that isengaged by a protrusion, flexible rod, or other such extension on thetool system.

The task coordination system 100 utilizes one or more UAVs to implementone or more tasks. As described above, the tasks can be substantiallyany relevant task that can be performed by one or more UAVs and/or oneor more tool systems cooperated with and/or transported by one or moreUAVs. In some implementations, one or more tasks may be scheduled andinitiated by the central control system 102. These tasks can includetasks that are regularly performed, tasks where timing of when a task isperformed may need to be controlled, tasks that are instructed by a userthrough the central control system, tasks the central control systemdetermines are to be performed based on sensor information, tasks that aUAV determines should be performed and is directed to be performedthrough the central control system, and other such tasks. The centralcontrol system can identify one or more UAVs and one or more toolsystems to be utilized to perform the one or more tasks. One or moreinstructions can be wired and/or wirelessly communicated by the centralcontrol system to one or more UAVs to direct the UAVs to cooperate withone or more tool systems, when the functionality is not alreadyavailable from the UAV or when a UAV does not have a relevant toolsystem with the needed functionality. Instructions can further beprovided to the one or more UAVs and/or relevant tool systems to beutilized in implementing the one or more tasks. The instructions, forexample, may specify timing, location of the task, location of a toolsystem, directions regarding how to perform the task, routing to befollowed in performing the task, and/or other such instructions.Further, in some applications, the central control system may evaluatepower levels of one or more UAVs and/or tool systems in selecting a UAVand/or tool system to be instructed to implement some or all of the taskor tasks. In some instances, tasks may be associated with a prioritylevel. Accordingly, some scheduled tasks may take priority over sometasks that a UAV determines should be performed, while in otherinstances one or more tasks that a UAV determines should be performedmay have priority over one or more scheduled tasks.

In some applications, the central control circuit may further evaluateinformation, such as sensor information, user entered data and/orinstructions, parameters and/or other such information in determiningwhether one or more tasks are to be performed. Similarly, in someembodiments, the UAV control circuit of one or more UAVs can beconfigured to identify one or more tasks to be performed and/or toolsystems to be used to perform one or more tasks. The UAV control circuitcan, for example, obtain sensor information from one or more externalsensors, internal sensors, sensors of one or more tool systemscooperated with the UAV, information from the central control system,information corresponding to a task or mission to be performed, and/orinformation from other sources in identifying one or more tasks to beperformed and/or the one or more tool systems to be used to perform thetasks. The UAV control circuit may apply internal analytics on relevantinformation to identify one or more tasks to be performed, and identifyone or more tool systems to be used to implement the one or more tasks.The analytics can include, for example, evaluating sensor data capturedby a first tool relative to one or more thresholds corresponding to thatsensor data, and identifying one or more predefined tasks that areassociated with the sensor data having a predefined relationship withthe one or more thresholds. For example, a sensor may detect thepresence of a threshold quantity of a predefined pest. The UAV controlcircuit and/or central control system may determine based on thedetection of the threshold quantity of the pest that a predefinedpesticide is to be applied. The UAV control circuit and/or centralcontrol system can identify one or more tool systems that can apply thepesticide over a determined area (e.g., which may also be based onlocation information associated with the sensor data detecting thepest). Similarly, the UAV control circuit and/or central control systemcan identify one or more UAVs to cooperate with the identified toolsystems and implement the task of applying the pesticide. Someembodiments may further direct instructions to one or more workers, suchas directing one or more workers to prepare a tool system. In the aboveexample, one or more workers may be directed to ensure a thresholdquantity of the pesticide is loaded into the one or more chemicalapplying tool systems.

In some embodiments, the UAV control circuit may identify a task to beperformed based at least in part on a current or previous task performedusing one or more tool systems that are temporarily coupled with theUAV. Further, the UAV control circuit may determine whether the task isto be performed by the UAV and/or one or more other UAVs. Additionally,the UAV control circuit can identify one or more tool systems to be usedto perform the task identified to be performed. For example, the UAV mayidentify that a subsequent task is needed to be performed based on acurrent task being performed by the UAV or tool system carried by theUAV. Similarly, a subsequent task may be identified based on informationreceived from a tool system being carried by another UAV. In someembodiments, the UAV control circuit may receive sensor data from a toolsystem carried by the UAV and obtained while performing a first task.Based on the sensor data received through the tool system, the UAVcontrol circuit can identify a second task and a second tool system tobe used in performing the second task.

When a different tool system is needed to perform the task, the UAVcontrol circuit may identify a location of the different tool system.The identification of a location of the different tool system may bethrough one or more databases storing information about tool systemidentifiers, corresponding functionalities and their current locations,and/or identification of a UAV with which the tool system is cooperated.The UAV may access the database, access information of a distributedledger, may communicate a request to the central control system 102 toprovide database information relative to the desired tool system,communicate with one or more other UAVs to identify locations of adesired tool system (e.g., a different UAV may respond that it iscarrying the desired tool system and/or it is aware of a mountingstation 114 where the desired tool system is located), and other suchsources.

As described above, at least some of the UAVs include the universalcoupler. Accordingly, in some instances, a UAV control circuit can causeand/or activate a decoupling of a first tool system from universalcoupler of the UAV, and direct the coupling of a different second toolsystem with the universal coupler following the decoupling of the firsttool system. In some instances the second tool system can be accessed atone of one or more mounting stations 114. The mounting station may beproximate to and/or within a geographic area being monitored by thesystem 100, while in other implementations may be remote from thegeographic area. The UAV control circuit can control the lift motors 204and propulsion systems 206 to direct the UAV to a mounting station totemporarily couple the universal coupler of the UAV with the second toolsystem, and subsequently control the propulsion system to direct the UAVto a task location and activate the second tool system in performing thesecond task.

The mounting station can include at least one tool docking station tosupport at least one tool system in a position that enables one or moreUAVs to cooperate with an intended tool system. Further, the mountingstation can be configured to store or support multiple different toolsystems as well as one or more empty tool docking station to receivetool systems that a UAV no longer needs. In some embodiments, the tooldocking station include an electrical coupling configured toelectrically couple with a tool system to supply power to the toolsystem and/or recharge an internal rechargeable power source 312 whileawaiting to be used and/or transported by a UAV. The mounting stationcan include a control circuit and/or one or more communicationtransceivers enabling the mounting station to further establish wiredand/or wireless communication with the tool system to enable retrievaland/or transfer of data (e.g., sensor data, image and/or video content,task parameters and/or history accumulated while performing a task(e.g., quantity of chemical dispensed, light exposure duration,ultrasound data, operation timing, etc.), other such data, orcombination of two or more of such data). Similarly, the mountingstation may be configured to establish wired and/or wirelesscommunication with a UAV. Some embodiments further include one or morecommunication couplers that are configured to physically couple with atleast one corresponding communication coupler on a tool system and/orUAV. Additionally, in some embodiments, the mounting station may furtherinclude one or more UAV docking stations configured to allow one or moreUAVs to temporarily dock with the mounting station to recharge one ormore rechargeable power sources of the UAV and/or to store the UAV whilenot in use.

The one or more tool systems mounted on a mounting station are typicallypositions to enable a UAV to cooperate with the tool system. In someembodiments, the task coordination system 100 includes one or moremounting stations 114 each configured to support at least one toolsystem at least while being cooperated with a UAV. Further, somemounting stations include one or more alignment systems that cooperatewith an alignment system of a UAV or universal coupler as at least oneof the UAV and a mounting station is moved to cause the cooperationbetween the alignment system of the UAV and the alignment system of themounting station to align at least a tool system with the universalcoupler enabling secure coupling between the UAV and the tool system.

In other instances, a UAV may obtain a tool system from another UAV. TheUAV control circuit of a first UAV and/or the central control system mayidentify one or more other UAVs carrying, having access to and/or beingat a position proximate to a tool system needed by the first UAV. TheUAV and/or central control system can communicate instructions to asecond UAV to disengage from the tool system and/or transport the toolsystem to a location and/or mounting station and disengage from the toolsystem. For example, the UAV control circuit of the first UAV mayidentify a second UAV temporarily coupled with the desired second toolsystem, and control the propulsion system to enable the first UAV toretrieve the second tool system from the second UAV. In still otherinstances, the disengagement of the second tool system from the secondUAV may occur only after the first UAV is in position to cooperate withthe second tool system. In some embodiments, the first UAV and secondUAV may exchange the tool system while in flight (e.g., the first UAVmay position itself and the universal coupler above the second UAV, andthe second UAV can release the tool system up to the first UAV).

Further, in some embodiments, the central control system 102 may directtwo or more UAVs to cooperatively perform a task. This cooperativeoperation may include two separate UAVs each cooperated with the samekind of tool system or different tool systems to cooperatively operateto perform parts of a task. For example, multiple UAVs may be directedto evaluate an area of crops in an attempt to identify and/or addressone or more types of insects or pests (e.g., tool systems to dispense achemical, tool system to emit a light at a predefined wavelength, etc.).As another example, two or more UAVs may be directed to utilize sensortool systems to obtain sensor data corresponding to a geographic area.Similarly, in some embodiments a UAV control circuit may identify thatat least a second UAV is to be used to cooperatively perform at least aportion of a task. This determination may be based on an amount ofgeographic area to be covered in performing the task, the quantity of amaterial to be applied to an area, a weight and/or size of a toolsystem, expected duration of time needed to perform the task, and/orother such factors. The UAV control circuit can cause a notification tobe communicated to the second UAV control circuit directing the secondUAV to perform at least the portion of the task in cooperation with thefirst UAV. Again, the second UAV may utilize the same or a differenttool system in cooperatively performing the task.

As a further example, in some embodiment a UAV control circuit of afirst UAV and/or the central control system may use sensor data obtainedfrom a first tool system carried by the first UAV and/or other sensordata from other sensors to detect a threshold level of infestation of apest. Based on the threshold level of infestation, the UAV controlcircuit and/or central control system can identify that at least apredefined quantity of pest repellant is to be applied to a known ordetermined geographic area of one or more crops. Further, based on thesize of the geographic area and quantity of repellant, a duration oftime can be predicted to apply the pest repellant to each of multiplesub-areas and identify a number of UAVs to be utilized to apply at leastthe pest repellant to the multiple sub-areas, which together cover thegeographic area, within an application threshold period of time (e.g.,want to apply the repellant within three hours to limit damagepotentially caused by the detected pest). Similarly, the UAV controlcircuit and/or central control system can select and direct the numberof UAVs to cooperate with a first type of tool system that includes apest repellant dispensing functional system with a reservoir to carrythe repellant and dispenser to dispense the repellant. In someinstances, further instructions can be provided regarding applyingsettings to the tool systems (e.g., rate of dispensing, pressure whendispensing, dispensing pattern (e.g., mist, stream, spray, fog, etc.),and/or other such settings) and/or UAV settings (e.g., altitude offlight during dispensing, route information to a sub-area, routeinformation while implementing the dispensing of the repellant, speed oftravel while dispensing, and/or other such settings).

In some embodiments, a UAV control circuit may continue to evaluatesensor data and/or other parameters (e.g., power level of the UAV and/ortool system, estimated percentage of completion of the task, remainingquantity of a chemical being applied, etc.) while implementing a task.Based on the sensor data and/or parameter information the UAV maydetermine that the UAV and/or a tool system will be unable to fullycomplete the task. Accordingly, the UAV control circuit may identifyanother UAV and/or tool system to take over to complete the task.Similarly, the UAV control circuit may notify the central control systemof the determination that the UAV and/or tool system will be unable tocomplete the task allowing the central control system to identify asubsequent UAV. In other implementations, the sensor data and/orparameters can additionally or alternatively be evaluated by the centralcontrol system to allow the central control system to predict that theUAV and/or tool system are unlikely to be able to complete the task andidentify a subsequent UAV and/or tool system.

In other instances, multiple UAVs may cooperatively operate inperforming a task with the multiple UAVs physically coupling togetherand/or multiple UAVs coupling with a single tool system. Some toolsystems, for example, may have a weight that exceeds a single UAV's liftcapacity and/or may have a size that limits a single UAV's ability toeffectively transport and/or utilize the tool system. Accordingly, thecentral control system and/or a UAV control circuit may direct multipleUAVs to cooperate to implement a task and/or utilize a tool system. Insome embodiments, a UAV control circuit of a first UAV can control thepropulsion system 206 to cause the first UAV to temporarily cooperatewith a universal coupler of a second UAV to allow the two UAVs tocooperatively perform at least a portion of a task. The universalcoupler of the first UAV can be configured to temporarily couple withanother universal coupler of a second UAV and maintain a position of thefirst UAV relative to the second UAV while the first UAV and second UAVare in motion. In some embodiments, the universal couplers of multipleUAVs can be utilized to couple multiple UAVs together and/or to create astack, train or chain of UAVs. In other instances, the universalcouplers of multiple UAVs may be temporarily secured with a cooperativecoupler or bridge structure that can include one or more additionaluniversal couplers to couple with one or more tool systems. Theuniversal coupler may include multiple coupling systems 216 to allow afirst coupling system to couple with a tool system and a second couplingsystem to couple with another UAV. Similarly, the orientation of thecoupling systems of one or more universal couplers on a UAV can bedirected down, up, toward a side, or other orientation depending on anintended implementation. FIGS. 2 and 4-5 illustrate the universalcoupler with a single coupling system 216 orientated downward to couplewith a tool system positioned underneath the UAV. In otherimplementations, however, the universal coupler may include a couplingsystem directed upward, laterally, or downward. In some instances auniversal coupler may include multiple coupler systems oriented indifferent directions.

In some embodiments, one or more tool systems may include a universalcoupler and/or second coupling system 316 to enable coupling with asecond UAV and/or another tool system. When cooperated with a secondtool system a single UAV may be able to simultaneously cooperate withmultiple tool systems (e.g., stacked, chained, etc.). Communicationbetween the UAV and the multiple tool systems may be through a daisychain coupling between the chained tool systems. In other embodiments, aUAV may include a specific coupler that is configured to secure with aspecific coupler of a tool system. This may restrict the use of sometool systems to being cooperated with specifically configured UAVs. Asdescribed above, in some embodiments, a UAV may include multipleuniversal couplers allowing multiple tool systems to simultaneouslycouple with the UAV, and/or a universal coupler may include multiplecoupling systems 216 that allows multiple tool systems to simultaneouslycouple with the single universal coupler.

Again, in some instances a task which may be performed by a single UAVor cooperatively performed by a plurality of UAVs may be scheduled,while in other instances the UAV control circuit may determine the taskto be performed based on sensor data and/or other information availableto the UAV control circuit. In some embodiments, the coordination ofmultiple UAVs to operate together and/or to physically couple to performone or more tasks may be coordinated by a UAV control circuit, betweenUAVs, by the central control system, or the like. The UAV controlcircuit of a first UAV, for example, may communicate directly with theUAV control circuit of a second UAV to coordinate the operation of boththe first UAV and the second UAV in performing at least a portion of oneor more tasks.

The task coordination system 100, in some embodiments, may include a UAVdatabase that is accessible to the central control system and/or one ormore UAV control circuits via the communication network 108. The UAVdatabase can store UAV capability data defining operational capabilitiesof each of the multiple UAVs, UAV historic information and/or other suchinformation. The UAV capabilities can include specification capabilitiesprovided by a UAV manufacturer (e.g., lift capabilities, flight durationcapabilities, size, communications capabilities, on-board sensors,flight speeds, other information, and typically a combination of two ormore of such information). Further the UAV database can store operatingcapacity and/or capabilities. The operating capabilities can includereal time data corresponding to conditions of the UAV, such as but notlimited to remaining battery power, current location information,current intended route information, tool system identifiers of one ormore tool systems cooperated with the UAV, estimated remaining flightcapabilities, altitude information, error data, operational statusinformation, sensor data from one or more internal UAV sensors, sensordata from one or more external sensors, other such capabilitiesinformation, or combination of two or more of such information. In someapplications, the UAV database may further include tool systemcapabilities corresponding to the one or more tool systems cooperatedwith the UAV (e.g., tool system power levels, fill level of one or morereservoirs, types of one or more sensors on the tool system, other suchinformation, or a combination of two or more of such information). TheUAV control circuit and/or the central control system can be configuredto access at least some of the UAV capability data and utilize thisinformation in making decisions regarding current and subsequent tasksbeing or to be performed. In some instances, for example, the UAVcapability data is utilized to select a set of one or more UAVs tocomplete a current task and/or at least initiate another task.

Some embodiments further include and/or have access to a tool systemdatabase configured to store tool system parameters associated with eachof a plurality of tool systems. The tool system parameters can, at leastpart, define a function that is performed by a corresponding one of theplurality of tool system. The tool system database can further storeoperating parameters, operating capabilities information, historicinformation, real-time current information, tool system identifiers,tool system locations, tool system capabilities corresponding to the oneor more tool systems cooperated with a UAV (e.g., tool system powerlevels, fill level of one or more reservoirs, types of one or moresensors on the tool system, other such information, or a combination oftwo or more of such information), other such information, or combinationof such information. The UAV control circuit and/or central controlsystem can access at least some of the tool system database in makingdecisions relative to one or more tool systems, such as selection of oneor more tool systems to be cooperated with each of one or more UAVs tobe used to implement the respective portions of one or more tasks.

Some embodiments further provide routing information to UAVs toimplement one or more tasks. The central control system and/or one ormore UAV control circuits can cause separate routing information to becommunicated to each of one or more UAVs to be followed whileimplementing respective portions of one or more task. The routing can bebased on the task to be performed, a geographic area or sub-area where aUAV is to implement a task, a current location of a UAV, a currentlocation of a tool system to be used by a UAV, power level of a UAVand/or tool system, and/or other such information. In some embodiments,a UAV control circuit obtains sensor data and based on the sensor dataidentifies a geographic area to be covered to implement one or moredetermined tasks. A number of UAVs to be utilized can be identified toimplement at least a portion of one or more of the tasks at thedetermined geographic location or sub-area of the geographic area.Timing information may also be identified, such as one or more thresholdperiod of times in which one or more tasks are to be performed.Notifications can be communicated to each of a set of one or more UAVsto implement at least a portion of one or more tasks relative to thegeographic location and/or one of the sub-areas.

Some embodiments further evaluate power levels of UAVs and/or toolsystems in selecting, directing and/or coordinating UAVs and toolsystems. In some implementations, a UAV control circuit may access powerlevel data corresponding to each of multiple other UAVs and select oneor more other UAVs from the multiple UAVs based at least in part on apower level of the one or more UAVs relative to one or more thresholdpower levels corresponding to task to be performed. Similarly, thecentral control system 102 may access the power level data and evaluatepower levels of different UAVs and/or tool systems in selecting and/orissuing instructions to one or more UAVs. The power level data may becommunicated by the UAVs and/or tool systems to the central controlsystem, a mounting station, a power tracking system, or the like. Inother embodiments, the power level information may be communicated byone or more UAVs and/or tool systems to other UAVs allowing UAVs tobuild local power level data. The communication of power levels may bebased on a schedule, based on one or more thresholds being meet (e.g.,stored power level drops below a power threshold), in response to aninquiry from another UAV or the central control system, other suchevents, or combination of two or more of such events.

As described above, in some embodiments, at least some tool systems mayinclude internal power sources (e.g., one or more batteries, capacitors,other such electrical power storage devices, or combination of two ormore of such devices). Further, in some implementations the power sourcemay be a rechargeable power source. For example, the tool system may berecharged while cooperated with a mounting station. In some embodiments,power may additionally or alternatively supplied by the UAV to a toolsystem temporarily cooperated with the UAV. This power may be used tooperate the tool system and/or recharge or partially recharge arechargeable power source of the UAV. Additionally or alternatively, aUAV may draw power from a tool system to further support the operationof the UAV and/or extend an operating time of the UAV. In someembodiments, the UAV control circuit and/or a power management system240 monitor power levels of one or more local rechargeable power sources212 on the UAV, and power levels of one or more power sources of a toolsystem. Power flow can be controlled by the UAV control circuitdepending on one or more thresholds, anticipated operating durations,external conditions, and/or other such information. Further, in someinstances, the power management system, which in some implementations isin communication with the UAV control circuit and in other instances isimplemented through the UAV control circuit, causes power to be drawnfrom and/or drained from one or more power sources 312 of a tool systemand stored in the rechargeable power source 212 of the UAV. In someapplications, the draining of the tool system power source is activatedprior to the tool system being decoupled from the UAV. For example, theUAV may cause the power source 312 to be drained in response tocompleting a task using the tool system, while in other instances, theUAV control circuit and/or power management system initiates thedraining of the power source 312 of the tool system upon approaching amounting station and/or upon docking a tool system with a mountingstation.

Some embodiments utilize multiple UAVs to cooperatively operate when atask or series of tasks are to be performed that may benefit by havingmultiple UAVs perform parts of the task or tasks. The multiple UAVs maycooperatively operate simultaneously in performing parts of the task. Inother implementations, one or more of the UAVs may sequentiallyoperation to cooperatively perform one or more tasks. In someembodiments, a UAV control circuit may evaluate data (e.g., sensor data,operating parameters, UAV parameters, tool system parameters, etc.) andidentify a task to be cooperatively performed by multiple UAVs (e.g.,the UAV performing the evaluation and one or more other UAVs). Sensordata may be obtained, and based on the sensor data a UAV control circuitmay identify a geographic area within which a task is to be implemented.A set of UAVs can be identified to be cooperatively utilized to eachimplement a portion of the identified task at a respective sub-area ofthe geographic area within a threshold period of time. One or morenotifications can be communicated to each of the set of UAVs torespectively implement at least a portion of the task relative to one ofthe sub-areas. A UAV control circuit may cause separate routinginformation to be communicated to each of the set of UAVs to be followedwhile implementing the respective portions of the task.

A UAV database may be maintained that stores UAV capability datadefining operational capabilities of each of the multiple UAVs. Thisdatabase may be maintained based on reporting statistics and/oroperational parameters received from UAVs and/or tool systems. The datamay be provided in response to an inquiry, based on threshold dataand/or other such events. One or more UAV control circuits can access atleast some of the UAV capability data and select, based on the UAVcapability data corresponding to a set of UAVs, a set of two or moreUAVs to cooperatively perform one or more tasks. Similarly, someembodiments additionally or alternatively maintain a tool systemdatabase storing tool system parameters associated with each of aplurality of tool systems and defining at least a function that isperformed by a corresponding one of the plurality of tool systems. Oneor more UAV control circuits can access at least some of the tool systemparameters to select, for each based on the tool system parameters, oneor more tool systems that are to be cooperated with each UAV of a set ofUAVs to be used by the set of UAVs to cooperatively implement respectiveportions of one or more tasks.

Some embodiments identify that multiple tool systems are to be used toimplement a task, a set of interrelated or dependent tasks, or the like.A set of tool systems can be selected from multiple available toolsystems. Similarly, a set of one or more UAVs can be selected to eachtemporarily cooperate with at least one of the multiple tool systems tobe used in cooperatively performing the task or tasks. In someinstances, one or more UAV control circuits may identify at least oneUAV in each of multiple geographic areas and communicate instructions toeach of the identified at least one UAV in each of multiple geographicareas directing each of the identified UAVs in each of multiplegeographic areas to perform one or more tasks within a respective one ofthe multiple geographic areas.

In some embodiments, the computation process to determine one or moretasks to be performed, identify one or more UAVs to utilize, identifyone or more tool systems to be utilized, routing, and/or other factorsmay be implemented through computational sharing across multiple UAVcontrol circuits. Some embodiments cause data acquired through a set ofone or more UAVs and/or tool systems can be accessed by UAV controlcircuits of one or more UAVs. Some of the data may be acquired whileperforming a set of at least one task. The data may be distributed to aset of two or more UAVs and/or two or more UAV control circuits areprovided access to the acquired data. The multiple UAV control circuitscan implement a cooperative computational processing of the data throughthe UAV control circuits and cooperatively identify based on thecooperative computational processing a set of at least one task to beperformed, and identify a set of at least two tool systems to beutilized by a set of UAVs in cooperatively performing the set of tasks.

In some implementations, a UAV control circuit may be designated aprimary control circuit and can issue instructions regarding thedistribution of the computational processing. In other implementations,the central control system can direct the distribution of computationprocessing between multiple UAV control circuits. Further, parameterdata may be accessed by the UAV control circuit to evaluate processingcapabilities of other UAV control circuits of other UAVs, currentprocessing being performed by other UAV control circuits of other UAVs,and other such parameters in selecting UAVs to be directed to performsome or all of the processing and/or determining how to distribute thecooperative computational processing. Further, one or more of the UAVsmay be in operation performing one or more tasks, while in someimplementations one or more or all of the UAVs performing the processingmay be in an idle mode (e.g., docked at a mounting or docking station,recharging station, simply waiting to be put into action, and/or othersuch idle modes). In some embodiments, UAV control circuits communicatestates and/or levels of processing. This reporting may be based on aschedule, based on a UAV control circuit reaching or maintaining aprocessing level greater than a processing threshold, in response to arequest for reporting, and/or other such instances. The reporting may bedirected to the central control system and/or a database, while in otherinstances the reporting may be directed to a particular UAV controlcircuit. In some implementations, however, the reporting may be relayedbetween UAV control circuits, allowing the information to be distributedover multiple if not all of the UAV control circuits within at least anoperating set of multiple UAVs. Further, the mounting stations maycomprise a mounting control circuit that can provide control over themounting station (and tool systems cooperated with the mountingstation). The mounting station control circuit may further be used as aresource in distributed computational processing. One or more UAVsand/or the central control system can direct instructions to a mountingstation to utilize computational resources of the mounting station inevaluating and determining tasks to be performed, whether notificationsshould be distributed (e.g., conditions require immediate action and/orattention by a human), whether and what type of tool system to be used,and/or other such distributed processing.

Further, some embodiments distribute information, parameters,assignments, scheduling, routing and/or other information betweenmultiple UAVs and/or tool systems. This can provide redundancy throughthe system as well as increase availability to information. One or moreUAVs and/or tool systems can be configured to maintain a copy ofinformation from one or more other UAVs and/or tool systems, providing abackup should one or more UAVs and/or tool systems fail, as well asfurther distributing the information and providing increasedaccessibility to that information. Additionally or alternatively, someembodiments utilize cloud based storage to distribute information,parameters, conditions, code, and/or other such information. In someembodiments, UAVs and/or tool systems can selectively clone itsinformation and/or attributes to one or more other UAVs, tool systems,central control system, cloud based storage, and/or other suchaccessible memory. Some embodiments utilize one or more shared,distributed ledgers or blockchain data schemes to facility informationdistribution, authenticate the transfer of information, and/or track thedistribution of information. The distributed ledger and/or blockchaindata schemes can further limit or prevent unauthorized access and/orhacking of the UAVs, tool systems and/or other information.

In some embodiments, UAV control circuits of one or more UAVs may accesscomputational processing capacity information associated with each ofthe multiple UAVs. The computational processing capacity may bemaintained in a processing capacity database, provided in response to arequest for current processing capacity, distributed based on aschedule, distributed in response to processing capacity exceeding ordropping below one or more thresholds and/or other such triggers. Theone or more UAV control circuits may use the processing capacityinformation to identify a set of at least two UAVs to be utilized inperforming the cooperative computational processing based on thecomputational processing capacity information associated with each ofthe set of the UAVs. The UAV control circuits in evaluating thecomputational processing capacity may identify UAV control circuits,mounting stations and/or the central control system having computationalcapacity that is greater than one or more capacity thresholds. The oneor more thresholds may be dependent on an expected type of computationalprocessing to be performed (e.g., evaluation of a first set of one ormore types of sensor data may require more computational processing anddatabase access than a second set of one or more types of sensor data,evaluation of multiple different types of sensor data be associated withother thresholds, thresholds based on a number of available resources(e.g., number of available UAVs in a given area over which a UAV istrying to make decisions, number of available tool systems, etc.), andother such considerations or factors).

As presented above, computational resources of multiple UAVs can becooperatively utilized to evaluation data and information in determiningtasks to be performed, selecting UAVs, selecting tool systems,scheduling tasks, routing UAVs and/or other such computationalprocessing. Some embodiments additionally utilize other computationalresources. For example, instructions can be communicated to a set of oneor more mounting stations directing each of the first set of mountingstations to access data, such as data acquired through one or more UAVsand/or tool systems, and further direct the set of mounting stations toimplement cooperatively computational processing of the data along withthe UAV control circuits of a set of one or more UAVs in cooperativelyidentifying a set of one or more tasks to be performed, cooperativelyidentify a set of at least two tool systems to be used to implement atleast part of a set of tasks, and/or other such processing. Additionallyor alternatively, some embodiments, communicate instructions to acentral control system directing the central control system to accessthe data acquired through one or more UAVs and/or tool systems, and toimplement cooperatively computational processing of the data along withthe UAV control circuits and/or a set of one or more mounting stationsin cooperatively identifying one or more task to be performed, identifya set of tool systems, determine routing by UAVs to implement the one ormore tasks, schedule the UAVs, and/or other such processing.

The distributed computational processing include the processing toidentify UAVs and/or tool systems based on geographic areas where tasksare to be performed and locations of UAVs and tool systems. In someembodiments, a UAV control circuit identifies at least one UAV in eachof multiple geographic areas. This may be in response to a query by theUAV control circuit, based on access to a location database, and/orother such information. Instructions in implementing the cooperativecomputational processing of data can be communicated to each of one ormore identified UAVs in each of multiple geographic areas directing eachof the identified at least one UAV in each of multiple geographic areasto perform at least a portion of the cooperative computationalprocessing to identify at least UAV, of a set of multiple UAVs, that isassociated with the respective one of the multiple geographic areas tobe activated in cooperatively performing at least one task. Similarly, aUAV control circuit may identify at least one UAV in each of multiplegeographic areas and communicate instructions, in implementing thecooperative computational processing of the data, to each identified UAVin each of multiple geographic areas directing each identified UAV ineach of multiple geographic areas to perform at least a portion of thecooperative computational processing to identify at least one toolsystem, of a set of tool systems, that is associated with the respectiveone of the multiple geographic areas to be utilized in cooperativelyperforming at least one task.

One or more UAV control circuits may access power level datacorresponding to each of multiple UAVs and/or tool systems, and selectUAVs and/or tool systems to be utilized in cooperatively performing atleast one task based at least in part on power levels of each of themultiple UAVs and/or tool systems relative to one or more thresholdpower levels corresponding to the task. In some embodiments, one or moreUAV control circuits access a UAV database storing UAV processingcapability data defining processing capabilities of each of the multipleUAVs, and select a set of at least two UAVs based on the processingcapabilities of each of the set of at least two UAVs.

As described above, in some implementations, UAV control circuitsidentify one or more tasks that a UAV is to perform. The determinationof a task to be performed may be based on a schedule, instructions froma central control system, instructions or request from another UAV,based on sensor information and/or parameter data acquired through theuse of one or more tool systems, other such factors, or a combination ofsuch factors. Similarly, a UAV may identify one or more types of toolsystems 106 to be used in implementing the one or more tasks and/or bedirected to utilize one or more types of tool systems. Based on the typeof tool system, a UAV control circuit can in some implementationsidentify a specific tool system of the type that is available for useand/or that may be made available for use. Again, one or more factorscan be considered in identifying or selecting a specific tool system tobe used. Some of the parameters may include, but are not limited to,distance between the UAV and the tool systems, stored power levels onthe tool systems, expected duration until a tool system is free for use,specific operating capabilities of the tool system (e.g., two toolsystems may both be configured to detect soil moisture but usingdifferent types of soil moisture sensors), other such parameters, andtypically a combination of two or more of such parameters.

In some embodiments, for example, a first UAV control circuit may beperforming a task using a tool system, and may determine that the firstUAV will be unable to complete the task. The first UAV may identify asecond UAV and/or send out a broadcast to determine which UAVs may beavailable. The second UAV can be notified and directed to take over thetask. Accordingly, the first and second UAVs can coordinate a handoff ofthe task to continue the task. In other instances, the task may be ascheduled prolonged task or a continuous task, and a second UAV cancontinue the task, and/or a tool system can be handed off between UAVsto perform the prolonged and/or continuous task.

In some embodiments, for example, a first UAV control circuit mayidentify a second UAV carrying a tool system that is configured toperform one or more functions that the first UAV control circuit hasdetermined needs to be performed and/or is instructed to perform.Further, the first UAV may identify that the second UAV has finishedusing the tool system or receive communication of when the second UAV isexpected to be finished with the tool system. The communication may bebased on a query from the first UAV to the second UAV, based onscheduling through the central control system, based on statusinformation accessible through one or more databased and/or distributedthroughout multiple UAVs, and/or other such methods. In some instances,the first UAV control circuit may cause a notification to becommunicated to the second UAV control circuit directing the second UAVto transfer the tool system to the first UAV. The transfer may bethrough a command and/or negotiation between the two UAVs directing thesecond UAV to dock the tool system at a selected mounting station (e.g.,closest mounting station to the second UAV, mounting station that isabout equidistant between UAVs, a selected mounting station based on alocation of the task to be performed, a selected mounting station basedon power levels of the two UAVs, and/or other such factors). In otherinstances, the transfer may be to merely direct the second UAV todeposit the tool system on the ground and direct the first UAV tosubsequently cooperate with the released tool system. In yet otherimplementations, the tool system may be transferred while both UAVs arein flight (e.g., second UAV carrying the tool system underneath thesubstructural support 208 can cooperate the tool system with a universalcoupler of the first UAV that enables coupling of a tool system on topof a substructural support; the first UAV may be configured to flyupside down for a period of time to cooperate with the tool system;etc.). Accordingly, the first UAV control circuit can direct thepropulsion system of the first UAV to the location of the tool systemand to position the first UAV to couple with the tool system beingtransferred from the second UAV.

In some embodiments, a UAV control circuit, in directing another UAV totransfer a tool system, may direct the other UAV to release the toolsystem at a location where a task is to be performed using the toolsystem. This can include directing the UAV to release the tool system onthe ground, in a mounting station proximate the area where the task isto be performed, placing the tool system and a predefined landing areaor other predefined deposit area, or the like. Similarly, someembodiments direct a second UAV to hover at a defined location andaltitude. A first UAV can direct its propulsion system to cause thefirst UAV to position the first UAV adjacent the second UAV and couplewith the tool system cooperated with the second UAV while the first UAVand the second UAV are in flight.

The determination that a tool system is to be handed off between UAVsmay be based on one or more factors. In some embodiments, for example, aUAV control circuit may identify a task being performed by another UAVusing a first tool system is to continue to be performed and/or is tocontinuously be performed. The UAV control circuit can direct itspropulsion system to couple with the first tool system and continueimplementing the task using the first tool system. Further, someembodiments identify a power level of a first UAV is less than athreshold power level. A notification can be communicated to the firstUAV directing the first UAV to transfer the tool system based on thepower level of the first UAV being less than the threshold power level.Similarly, some embodiments evaluate a power level of a tool system toconfirm that there is sufficient power in the tool system to continuebeing used to perform a task. Accordingly, some embodiments confirm apower level of a tool system is greater than a tool system power levelthreshold prior to causing the notification to be communicated to a UAVdirecting the UAV to transfer the tool system.

Some embodiments evaluate location data of a tool system and/or UAVsprior to initiating a transfer in attempts to reduce delay, reduce powerdrain due to at least extended travel, and/or other such factors. A toolsystem database may be maintained storing tool system parameter dataassociated with each of multiple tool systems. The database may, inpart, define functional capabilities and current location of each of themultiple tool systems. UAV control circuits can be configured to accessthe tool system database, identify one or more tool systems has afunctionality to be used to perform a task, and identify that at leastone of the one or more tool systems is within a threshold distance ofthe UAV that is to temporarily couple with the intended tool system. Insome embodiments, tasks may have time restrictions. As such, toolsystems may be transferred in attempts to complete tasks withinthreshold time limits. A UAV control circuit may identify that a secondUAV is predicted to complete a first task being performed using thefirst tool system within a threshold period of time.

Other triggers and/or conditions can be detected to cause a transfer ofone or more tool systems. Some embodiments, for example, can initiate atransfer of a tool system based on tool conditions, which may beprojected (e.g., based on the task being performed, time spentperforming the task, predicted remaining time to complete the task, typeof tool parts, etc.) and/or measured. Similarly, the transfer of a toolsystem may be based on a knowledge of schedule tasks performed sincelast maintenance and projection or future wear rates for tasks planned.Historic tools experience wear and tear, maintenance, cleaning,charging, re-filling, sharpening, etc. can be considered. In someinstances, a tool system hand-off may be initiated based on detectableand/or observable characteristics.

Some embodiments evaluate the conditions of tool systems in determiningwhether to initiate a tool system transfer. Measured and/or predictedconditions and observations about tool system conditions can be madefrom one or more sensor inputs, from integrated system performancemonitoring (e.g., such as a force or time needed to perform a taskincreases with wear), and/or other such conditions. For example, a toolsystem control circuit, a UAV control circuit and/or the central controlsystem may track progress of a tool system performing a task andevaluate progress based on one or more thresholds (e.g., cutting with adull blade takes longer, increased pressure is needed, etc.) which areoften detectable and/or observable. Other detectable characteristics canbe used depending on the specifics of the tool system (e.g., low tankwhen the tool system includes a tank carrying a chemical or othersubstance), change in weight when dispensing or collecting, etc.).

Some embodiments in selecting UAVs to perform a task and/or selecting atool system to be used may further consider power levels of UAVs and/ortool systems. Further, some embodiments attempt to balance powerutilization between UAVs and/or tool systems. In some embodiments, a UAVcontrol circuit of a UAV and/or the central control system may accesspower level data corresponding to each of multiple different UAVs of atask coordination system 100. The power level data may be received fromUAVs and/or tool systems based on a schedule, based on a notification inresponse to a power level dropping below each of one or more thresholds,based on a request communicated to UAVs and/or tool systems from arequesting UAV control circuit and/or central control system, or thelike. For example, a UAV control circuit may cause one or more powerlevel polling requests to be communicated and/or broadcasted to multipleUAVs and/or tool systems, and receive power level information based onthe polling request. One or more power databases may be maintained, forexample by the central control system, that includes power level dataassociated with multiple UAVs and/or tool systems. UAVs and/or toolsystems may communicate power level data to the central control systems,which can update power levels in the power database. As described above,the power level data may be communicated based on a schedule, thresholdsand/or other such conditions or events. UAV control circuits and/or thecentral control system can access power level information from the powerdatabase in evaluating UAVs and/or tool systems.

In some embodiments, power demands and/or expected power usage toperform a task can be determined and/or accessed. For example, a task tobe performed and a corresponding tool system to be used in performingthe task can be identified. A predicted power usage can be determinedbased on the task to be performed, an area to be traveled to cooperatewith a tool system and performing the task can be predicted, parameterscan be considered (e.g., wind speed, temperature, humidity, aerialand/or ground traffic in or within threshold distance of an area wheretask is to be performed, presence of humans, and/or other suchparameters), and/or other such factors can be considered. Based onexpected power usage information and the power level data of UAVs and/ortool systems, one or more other UAVs can be selected based at least inpart on a power level of the one or more other UAVs relative to one ormore threshold power levels corresponding to a task to be performed anda predicted power usage of the UAV and/or one or more tool systems to betemporarily cooperated with the one or more UAVs to be used inperforming the task. Further, some embodiments may use multiple UAVs inperforming a set of different tasks and rotate the multiple UAVs betweenthe different tasks to balance power usage. This may include switchingbetween different tool systems to perform the different tasks. Further,the balancing of power may include switching between different UAVswhile allowing UAVs to recharge before switching back into a rotation ofmultiple UAVs directed to perform one or more tasks.

Some embodiments include a power level database maintaining power leveldata of each of the multiple UAVs and/or tool systems that can beaccessed by UAV control circuits. Additionally or alternatively, someembodiments may include a task predicted power usage databaseassociating for each of the multiple UAVs predicted power usage datacorresponding one of the UAVs to carry at least a selected one ofmultiple tool systems to perform at least one of multiple differenttasks. UAV control circuits can access the task predicted power usagedatabase to identify a predicted amount of power to be utilized by eachof at multiple UAVs to perform a task. Further, a UAV control circuitmay access the power level database, and evaluate the power level dataindicating a current power level of each of multiple UAVs relative tothe predicted amount of power to be utilized by the corresponding UAV.

In some embodiments, a UAV control circuit is configured to determine apredicted amount of power that a second UAV is predicted to utilize tocarry a first tool system to perform a task. In some instances, theprediction of power usage may include identifying a predicted distanceof travel by the UAV in performing the task. Similarly, some embodimentsaccess predicted power usage by two or more of multiple tool systems toperform a task, and select a tool system of the multiple tool systemsbased at least in part on a power level of the tool system relative to atool system threshold power level corresponding to the task to beperformed and a predicted power usage by the tool system in performingthe task. The predicted power usage may be based on specifications ofthe UAVs and/or tool systems, based on historic data corresponding tothe same or similar UAV and/or tool system being used to perform thesame or similar tasks, and/or other such information. For example, insome embodiments UAV control circuits cause power levels and/or usagedata to be communicated to the central control system that can maintaina power level data. Using this information the central control circuitcan determine power usage relative to various factors (e.g., type ofUAV, type of tool system used, number and/or type of tool systemscooperated with a UAV, tool system parameters (e.g., size, weight, winddrag, etc., quantity of chemical carried), type of task performed,duration of performing the task, other such factors, or combination oftwo or more of such factors). Further, one or more thresholds may beassociated with data. For example, some data may not be consideredunless one or more thresholds are met (e.g., threshold change in powerlevel, threshold duration of operation, etc.).

One or more UAV control circuits may be configured to direct acooperative operation of each of the multiple UAVs in performing a setof different tasks and rotate the two or more of the multiple UAVsbetween the different tasks to balance power usage between the multipleUAVs. For example, a first tool system may be relatively heavy compartedto one or more other tool systems. Accordingly, multiple UAVs may bedirected to switch tool systems while performing one or more tasks tobalance power usage by the UAVs and/or provide an extended performanceof the one or more tasks. Similarly, a tool system may draw power from aUAV. Accordingly, multiple UAVs may be directed to switch tool systems.In some applications, different tasks may result in greater powerdrains. For example, some tasks may take longer to perform. Accordingly,multiple UAVs may be cooperatively directed to perform a task inattempts to balance power usage.

In some embodiments, the central control system evaluates power levelusage relative to historic power level usage information in evaluatingan efficiency of operation of the multiple UAVs, evaluate UAVsperformance and/or potential need for maintenance, track deterioratingperformance of a UAV and/or tool system in adjusting expected powerusage for that UAV and/or tool system, and/or other such considerations.Further, in some instances, power management can direct a UAV to drainpower from a power source of a tool system cooperated with the UAV andbe stored in a power source of the UAV prior to the UAV disengaging fromthe tool system. Some embodiments further identify one or more sensorsystems and/or tool systems that are not currently and/or predicted tobe needed, and direct the UAV to power down those systems, and whererelevant to decouple from those systems. The decoupling may result inreduced weight and thus provide greater expected efficiency and/orincrease operational time.

The predicted power usage may be based on historic information usingpower usage data obtained when one or more UAVs and/or tool systems wereused to perform the same or similar tasks, considering effects ofsimilar parameters (e.g., similar wind speeds, expected aerial and/orground traffic, etc.), consideration of power usage when performing thesame or different tasks over similar amounts of areas to be traversed,and/or other such information. Some embodiments further maintain orstore power level usage over time of the selected one or more UAVsand/or tool systems to be utilized in subsequent power balance analysis.Still further, some embodiments may evaluate power usage relative tohistoric power level usage information in evaluating the efficiency ofoperation of one or more UAVs and/or tool systems, evaluate UAVsperformance and/or potential need for maintenance, track deterioratingperformance of a UAV and/or tool system in adjusting expected powerusage for that UAV and/or tool system, and/or other such considerations.For example, the central control system and/or a UAV control circuit mayidentify that a quantity of power usage to perform one or more tasksexceeds a threshold and direct that maintenance be performed on the UAVand/or tool system (e.g., replace a rechargeable power source, perform acleaning, perform a sharpening of parts of a tool system, etc.).

Further, some embodiments maintain and provide access to one or moreshared, distributed ledgers or blockchain data schemes. Informationacquired through one or more UAVs and/or tool systems may becommunicated using chained blocks and a distributed ledger keptregarding the communications. The distributed ledger can be replicatedamong multiple communication systems and/or devices (e.g., UAVs, toolsystems, mounting stations, docking stations, central control system,and/or other such communication systems). Some or all of the distributedledger may be a private, while some or all of the distributed ledger maybe a public scheme. The ledger entries blocks may apply a proof-of-work,proof-of-stake, proof-of-space, and/or other such authentication toachieve distributed consensus. The private ledgers may apply restrictedaccess to authorized systems or devices. The ledger can provide accessto information (e.g., sensor information, scheduling, operating statusinformation (e.g., power levels, tool systems in use, estimatedpercentage of a task completed, etc.), available and in use UAVs andtool systems information, location information of UAVs and tool systems,mounting station locations, availability to receive tool systems atmounting stations, history of completed tasks, history of user inputs,history of user requests, history of UAVs operations, history of toolsystem operations, other such information, and typically a combinationof two or more of such information). Further, the ledger information canbe accessed by multiple systems of the task coordination system 100. Insome instances, information from a UAV and/or tool system is uploaded ina batch when returned to a mounting station and/or docking station.

The tool systems, as described above, enable the task coordinationsystem 100 to utilize UAVs to perform multiple different tasks. The UAVsdo not have to be built to perform specific tasks, but instead can beassembled with one or more couplers and/or the universal coupler toenable the different UAVs to releasably cooperate with one or more toolsystems that can be carried by the UAVs to a location where the toolsystems are to be utilized. In some instances, for example, one or moretool systems can be utilized to track crops over one or more areas. Thecrop tracking and/or monitoring can be through image and/or videoprocessing, image comparisons between images captured at differenttimes, pest detection, soil sampling, crop ripeness evaluation (e.g.,through light and/or optical processing), and/or other such monitoring.

In some embodiments, one or more tool systems can be configured todetect RFID tags, watermarks and/or other such distinguishing marks oridentifiers. Workers and/or one or more tool systems can be utilized totag test crops, such as with RFID tags, watermarking, or other suchtagging. UAVs can carry appropriate tool systems over relevant areas todetect the tagged crops and monitor test crops and/or one or more testplants within a test crop, for any number of parameters such as, forexample, fruit development, sugar content of fruit, ripening of fruit,insect resistance, moisture levels, and/or others such parameters. Suchparameters may be determined based on video sampling, moisture sampling,fruit sampling and testing at a site, and other such informationacquisition. One or more tool systems may be utilized to captureinformation to enable evaluation of one or more of these parameters.Accordingly, the task coordination system allows remote monitoring ofcrops, plants, test crops, test plants, infestations, soil conditions,weather, and other items, conditions, projects and the like.

Some tool systems may be configured to support and/or assist other toolsystems. For example, some tool systems may provide replacementcomponents, retrieve samples taken by another tool system, transport apayload to or from another tool system, and/or provide other services toa tool system. As further examples, an assistant tool system maycarrying a replacement bulb for a lighting tool system, an assistanttool system may replace a drill bit or saw of a drilling or sawing toolsystem, an assistant may supply one or more additional sensors to beplaced by another drown, an assistant tool system may provide additionaltreatment chemicals or materials, an assistant tool system may transportone or more additional treatment containers and/or retrieve one or moretreatment containers with samples from a sampling tool system, and/orother such assistance functions.

Further, the circuits, circuitry, systems, devices, processes, methods,techniques, functionality, services, servers, sources and the likedescribed herein may be utilized, implemented and/or run on manydifferent types of devices and/or systems. FIG. 6 illustrates anexemplary system 600 that may be used for implementing any of thecomponents, circuits, circuitry, systems, functionality, apparatuses,processes, or devices of the above or below mentioned circuitry, systemsor devices, or parts of such circuits, circuitry, functionality,systems, apparatuses, processes, or devices. For example, the system 600may be used to implement some or all of central control system 102, UAVs104, tool systems 106, mounting stations 114, service requestors 122,UAV control circuits 202, tool system control circuits 302, and/or othersuch components, circuitry, functionality and/or devices. However, theuse of the system 600 or any portion thereof is certainly not required.

By way of example, the system 600 may comprise a control circuit orprocessor module 612, memory 614, and one or more communication links,paths, buses or the like 618. Some embodiments may include one or moreuser interfaces 616, and/or one or more internal and/or external powersources or supplies 640. The control circuit 612 can be implementedthrough one or more processors, microprocessors, central processingunit, logic, local digital storage, firmware, software, and/or othercontrol hardware and/or software, and may be used to execute or assistin executing the steps of the processes, methods, functionality andtechniques described herein, and control various communications,decisions, programs, content, listings, services, interfaces, logging,reporting, etc. Further, in some embodiments, the control circuit 612can be part of control circuitry and/or a control system 610, which maybe implemented through one or more processors with access to one or morememory 614 that can store instructions, code and the like that isimplemented by the control circuit and/or processors to implementintended functionality. In some applications, the control circuit and/ormemory may be distributed over a communications network (e.g., LAN, WAN,Internet) providing distributed and/or redundant processing andfunctionality. Again, the system 600 may be used to implement one ormore of the above or below, or parts of, components, circuits, systems,processes and the like. For example, the system may implement thecentral control system 102 with the control circuit being a centralsystem control circuit, a UAV 104 with the UAV control circuit 202, atool system 106 with a tool system control circuit 302, or othercomponents.

The user interface 616 can allow a user to interact with the system 600and receive information through the system. In some instances, the userinterface 616 includes a display 622 and/or one or more user inputs 624,such as buttons, touch screen, track ball, keyboard, mouse, etc., whichcan be part of or wired or wirelessly coupled with the system 600.Typically, the system 600 further includes one or more communicationinterfaces, ports, transceivers 620 and the like allowing the system 600to communicate over a communication bus, a distributed computer and/orwired and/or wireless communication network 108 (e.g., a local areanetwork (LAN), the Internet, wide area network (WAN), etc.),communication link 618, other networks or communication channels withother devices and/or other such communications or combination of two ormore of such communication methods. Further the transceiver 620 ormultiple transceivers can be configured for wired, wireless, optical,fiber optical cable, satellite, or other such communicationconfigurations or combinations of two or more of such communications.Some embodiments include one or more input/output (I/O) ports 634 thatallow one or more devices to couple with the system 600. The I/O portscan be substantially any relevant port or combinations of ports, such asbut not limited to USB, Ethernet, or other such ports. The I/O interface634 can be configured to allow wired and/or wireless communicationcoupling to external components. For example, the I/O interface canprovide wired communication and/or wireless communication (e.g., Wi-Fi,Bluetooth, cellular, RF, and/or other such wireless communication), andin some instances may include any known wired and/or wirelessinterfacing device, circuit and/or connecting device, such as but notlimited to one or more transmitters, receivers, transceivers, orcombination of two or more of such devices.

In some embodiments, the system may include one or more sensors 626 toprovide information to the system and/or sensor information that iscommunicated to another component, such as the tool system controlcircuit, UAV control circuit, central control system, etc. The sensorscan include substantially any relevant sensor, such as distancemeasurement sensors (e.g., optical units, sound/ultrasound units, etc.),motion sensors, inertial sensors, location sensors, and other suchsensors. The foregoing examples are intended to be illustrative and arenot intended to convey an exhaustive listing of all possible sensors.Instead, it will be understood that these teachings will accommodatesensing any of a wide variety of circumstances in a given applicationsetting.

The system 600 comprises an example of a control and/or processor-basedsystem with the control circuit 612. Again, the control circuit 612 canbe implemented through one or more processors, controllers, centralprocessing units, logic, software and the like. Further, in someimplementations the control circuit 612 may provide multiprocessorfunctionality.

The memory 614, which can be accessed by the control circuit 612,typically includes one or more processor readable and/or computerreadable media accessed by at least the control circuit 612, and caninclude volatile and/or nonvolatile media, such as RAM, ROM, EEPROM,flash memory and/or other memory technology. Further, the memory 614 isshown as internal to the control system 610; however, the memory 614 canbe internal, external or a combination of internal and external memory.Similarly, some or all of the memory 614 can be internal, external or acombination of internal and external memory of the control circuit 612.The external memory can be substantially any relevant memory such as,but not limited to, solid-state storage devices or drives, hard drive,one or more of universal serial bus (USB) stick or drive, flash memorysecure digital (SD) card, other memory cards, and other such memory orcombinations of two or more of such memory, and some or all of thememory may be distributed at multiple locations over the computernetwork 108. The memory 614 can store code, software, executables,scripts, data, content, lists, programming, programs, log or historydata, user information, customer information, product information, andthe like. While FIG. 6 illustrates the various components being coupledtogether via a bus, it is understood that the various components mayactually be coupled to the control circuit and/or one or more othercomponents directly.

FIG. 7 illustrates a simplified flow diagram of an exemplary process 700of performing tasks through multiple UAVs, in accordance with someembodiments. In step 702, a UAV control circuit implements aninstruction to temporarily couple with a tool system 106 of multipledifferent tool systems that are each configured to perform a differentfunction to be put into use while or after being carried by one of theplurality of UAVs. For example, a tool system may comprise a packagesecuring tool system configured to retain and enable transport of apackage while being delivered, a sensor tool system configured to sensea condition and communicate sensor data of the sensed condition to theUAV control circuit, a lighting tool system, one or more cameras, motionsensors, other such functions, or combination of two or more of suchfunctions.

In step 704, a propulsion system of the UAV is controlled to align auniversal coupler 214 of the UAV with a tool system. As described above,the universal coupler is configured to interchangeably couple with anddecouple from one of multiple different tool systems. In step 706, acoupling system of the universal coupler is caused to securely couplewith the tool system, and enables a communication connection between acommunication bus 220 of the universal coupler and the tool system 106.

Some embodiments, in aligning the universal coupler with the toolsystem, further control the movement of the UAV such that a first set ofpermanent magnets 406 of the UAV are in a threshold distance of a secondset of permanent magnets 408 of the tool system and enable a magneticinteraction between the first set of permanent magnets and the secondset of permanent magnets. In some embodiments, the UAV and/or the toolsystem may include one or more sets of electromagnets. A decoupling canbe implemented between the UAV and the tool system by activating one ormore sets of electromagnets. In some instances, one or moreelectromagnets may be positioned relative to one or more sets ofpermanent magnets and activated in part to overcome a magnetic forcerelative to at least the permanent magnet.

Further, the aligning of the universal coupler with a tool system mayinclude engaging an alignment structure of the UAV and/or universalcoupler with at least an alignment structure of the tool system as atleast one of the tool system and the UAV are moved, and enabling acoupling to be implemented between the UAV and the tool system. Theengagement between the alignment structure of the UAV and/or universalcoupler with the alignment structure of the tool system can includecausing one or more generally cone shaped cavities of the alignmentstructure of the UAV and/or universal coupler to align with and/orengage one or more generally cone shaped protrusions of the alignmentstructure of the tool system, and/or one or more cone shaped cavities ofthe tool system with one or more cone shaped protrusions of theuniversal coupler. Other embodiments may additionally or alternativelyuse different shaped cavities and protrusions to aid in aligning thetool system and the universal coupler such as but not limited to domeshaped, pyramid shaped, and/or other such shapes. Some embodiments mayfurther induce air flow, suction, and/or other methods to assist inalignment.

A coupling system of a universal coupler may include a gripping systemthat can be activated to grip a grip feature of the tool system. Someembodiments securely couple the coupling system with the tool system byextending the gripping system of the UAV and/or the universal coupler toa position to grip the grip feature. The gripping system may, in someinstances, be retracted to secure the tool system with the universalcoupler. In securing the coupling system, some embodiments cause one ormore extensions of the UAV, universal coupler and/or tool system toengage a recess formed in a surface of a mating protrusion of the toolsystem, or universal coupler. The extension may assist in aligning andinhibiting rotation of the tool system while the gripping system isretracted a threshold distance.

The alignment between the universal coupler and a tool may includecausing one or more alignment structures of the UAV to engage with oneor more alignment structures of a mounting station of multiple mountingstations. At least some of the mounting stations are typicallyconfigured to support and align at least one tool system as one of a UAVand a mounting station are moved to cause the engagement between thealignment structures of the UAV and tool system to align the tool systemenabling secure coupling between the UAV and the tool system. In someembodiments, universal couplers can be configured to coupler to one ormore other universal couplers. Some embodiments control the propulsionsystem of a first UAV and align a first universal coupler of the firstUAV with a universal coupler of a second UAV, and cause a couplingsystem of the first universal coupler to securely couple with theuniversal coupler of the second universal coupler to maintain a positionof the first UAV relative to the second UAV while the first UAV andsecond UAV are in motion and while at least one or more tool systems areactive.

FIG. 8 illustrates a simplified flow diagram of an exemplary process 800of performing tasks through multiple UAVs, in accordance with someembodiments. In step 802, data obtained through a first tool systemtemporarily coupled with a universal coupler of a UAV, while performinga first task using the first tool system, is accessed and/or obtain bythe UAV control circuit. In step 804, one or more other tasks areidentified, through the UAV control circuit and based at least in parton the accessed data, that is to be performed by the UAV. In step 806,one or more tool systems are identified, through the UAV control circuitand based on the second task to be performed, that are to be used toperform the second task. Some embodiments in accessing the data receivesensor data from the first tool system obtained while performing thefirst task. The one or more other tasks to be performed and the one ormore tool systems to be used may be identified based on the sensor datareceived through the first tool system.

In some embodiments, a decoupling of the first tool system from auniversal coupler of the UAV is caused. The decoupling may be activatedby the UAV control circuit. In some instances, the first tool system maybe secured with the universal coupler through one or more couplers thatmay be activated and deactivated. For example, retractable pins may beretracted, a lever arm may be rotated, one or more electromagnets may beactivated or deactivated, other such decoupling, or combination of twoor more of such decoupling may be implemented. The coupling of a secondtool system can be directed with the first universal coupler followingthe decoupling of the first tool system.

Some embodiments control a propulsion system of the first UAV directingthe first UAV to a first mounting station. The second tool system istemporarily coupled with a first universal coupler of the first UAV. Thepropulsion system can further be controlled to direct the first UAV to atask location and activating the second tool system in performing thesecond task. In other instances, a second UAV temporarily coupled withthe second tool system may be identified, and the propulsion system ofthe first UAV can be controlled to retrieve the second tool system fromthe second UAV.

In some instances, the UAV control circuit of the first UAV can identifyone or more other UAVs that are to be used to perform at least a portionof the second task. A notification can be caused to be communicated tothe one or more other UAVs directing the one or more other UAVs toperform at least the portion of the second task in cooperation with thefirst UAV. This can allow a team of UAVs to cooperatively perform one ormore tasks. Some embodiments control a propulsion system of the firstUAV to cause the first UAV to temporarily cooperate with a universalcoupler of a second UAV while perform at least the portion of a task. Insome embodiments, the UAV control circuit of the first UAV accessespower level data corresponding to each of multiple other UAVs, andselects one or more other UAVs from the multiple UAVs based at least inpart on a power level of the one or more other UAVs relative to athreshold power level corresponding to the second task. The UAV controlcircuit of the first UAV can initiate a direct communication with thesecond UAV to coordinate the operation of both the first UAV and thesecond UAV in performing at least a portion of one or more tasks. Insome instances, power can be drained from a power source of the firsttool system and stored in a power source of the first UAV prior to thefirst tool system being decoupled from the first UAV.

FIG. 9 illustrates a simplified flow diagram of an exemplary process 900of managing tasks through the cooperative operation of multiple UAVs, inaccordance with some embodiments. In step 902, data is accessed that isobtained through one or more tool systems temporarily coupled with oneor more UAVs while performing one or more tasks using the one or moretool systems. In step 904 a set of at least one task is identified thatis to be cooperatively performed by a set of multiple UAVs. In someinstances, a UAV control circuit can evaluate the accessed and based atleast in part on the data identify the set of at least one task to becooperatively performed by the set of UAVs. In step 906, one or moreUAVs of multiple UAVs are identified that are to be activated to performthe set of at least one task in cooperation with a first UAV.

The cooperative operation of UAVs may, in some instances, be based atleast in part on geographic areas. Sensor data may be accessed, andbased on the sensor data one or more geographic areas can be identifiedwithin which a set of at least one task is to be implemented. A set ofUAVs can be identified to be cooperatively utilized to each implement aportion of the set of at least one task at a respective sub-area of thegeographic area within a threshold period of time. The set of UAVs maybe identified based on their current location being within a thresholddistance of a geographic area, or sub-area. In other instances, UAVs maybe selected to route to different areas or sub-areas based on toolsystems cooperated with UAVs and/or tool systems within thresholddistances of the UAVs. Notifications can be communicated to each of theset of UAVs to respectively implement at least a portion of the set ofat least one task relative to one of the sub-areas. Further, someembodiments cause separate routing information to be communicated toeach of the UAVs to be followed to get to an area or sub-area, and/or tobe followed while implementing the respective portions of the set of atleast one task.

Some embodiments maintain UAV capability data in a UAV database thatstores and defines operational capabilities of each of multiple UAVs.Multiple UAVs may be selected, based on the UAV capability datacorresponding to a set of UAVs, to cooperatively perform a set of atleast one task. Similarly, some embodiments maintain tool systemparameters in a tool system database associating storing tool systemparameters with each of a plurality of tool systems and defining atleast one or more functions that are performed by a corresponding one ofthe plurality of tool systems. The operational capabilities may furtherdefine operating durations, power level capacity, current power levels,specifications, levels of performance, efficient information, currentlocation information, and/or other such information. The tool systemdatabase may be access and a tool system may be selected, based on thetool system parameters for each of the multiple selected UAVs, that isto be cooperated with one of the multiple UAVs to be used to implementrespective portions of the set of at least one task.

Some embodiments identify that multiple tool systems are to be used toimplement the set of at least one task, and can select from multipleavailable tool systems a set of two or more tool systems to be utilized.Similarly, a first set of UAVs may be selected, from multiple UAVs, thatare to each to temporarily cooperate with at least one of the selectedtool systems to be used in cooperatively performing the set of at leastone task. Geographic information may further be taken into considerationin selecting UAVs and/or tool systems. In some applications, at leastone UAV is identified in each of multiple geographic areas. Instructionscan be communicated to each of the identified UAVs in each of multiplegeographic areas directing each of the identified UAVs in each ofmultiple geographic areas to perform a set one or more tasks within arespective one of the multiple geographic areas.

FIG. 10 illustrates a simplified flow diagram of an exemplary process1000 of performing distributed computational processing across multipleUAVs, in accordance with some embodiments. In step 1002, data acquiredthrough at least a first set of at least one UAV while performing afirst set of one or more tasks is distributed to a second set of atleast two UAVs. In step 1004, cooperative computational processing ofthe data is implemented through UAV control circuits of the second setof UAVs. In step 1006, second set of one or more tasks that are to beperformed are identified based on the cooperative computationalprocessing. In step 1008, a set of at least two tool systems areidentified that are to be utilized by a third set of at least two UAVsin cooperatively performing the second set of tasks.

Computational processing capacity information can be accessed that isassociated with each of multiple UAVs. A set of UAVs can be identifiedto be utilized in performing the cooperative computational processingbased on the computational processing capacity information associatedwith each of the second set of the at least two UAVs. Some embodimentsmaintain a UAV database and/or a computational processing database thatcan maintain current information regarding processing total potentialcapabilities, currently utilized processing capability bandwidth (whichmay be based on an average processor usage and/or historic usage over aperiod of time, scheduled processing, predicted processing, and/or othersuch information), tool system processor demands, sensor data processingdemands, and/or other such processing. Mounting stations mayadditionally or alternatively be used in computational sharing. In someinstances, instructions can be communicated to a set of one or moremounting stations directing each of the set of mounting stations toaccess at least data acquired through a set one or more UAVs. Theinstructions cause the cooperatively computational processing of thedata by the set of mounting stations, which may be along with processingby one or more UAV control circuits of a set of UAVs in cooperativelyidentifying a set one or more tasks to be performed and a correspondingset of tool systems to be utilized in implementing one or moreidentified tasks. Some embodiments communicate instructions to thecentral control system directing the central control system to accessthe data acquired through at least the first set of at least one UAV,and causing the cooperatively computational processing of the data bythe central control system along with the UAV control circuits of theset of UAVs and/or the set of mounting stations in cooperativelyidentifying the set of task to be performed and the set of tool systems.

The cooperative computational processing may be distributing in partbased on geographic areas. One or more UAVs may be identified in each ofmultiple geographic areas. Instructions can be communicated to each ofthe identified UAVs in each of multiple geographic areas directing theUAVs in each of multiple geographic areas to perform at least a portionof the cooperative computational processing to identify at least oneUAV, of a set of multiple UAVs, that is associated with the respectiveone of the multiple geographic areas to be activated in cooperativelyperforming a set of tasks. Similarly, some embodiments identifying oneor more UAVs in each of multiple geographic areas, and communicateinstructions to each of the identified UAVs directing each of the UAVsin each of multiple geographic areas to perform at least a portion ofthe cooperative computational processing to identify at least one toolsystem, of a set of tool systems, that is associated with the respectiveone of the multiple geographic areas to be utilized in cooperativelyperforming a set of one or more tasks. Further, some embodiments incausing the cooperative computational processing cause a UAV controlcircuit of each of the set of UAVs to access power level datacorresponding to each of multiple other UAVs, to select at least onetool system of the set of tool systems and selecting at least one UAV tobe utilized in cooperatively performing one or more tasks based at leastin part on power levels of each of the multiple other UAVs relative toone or more threshold power level corresponding to at least one of thetasks. One or more UAV databases and/or processing capabilitiesdatabases may be maintained and accessed that store UAV processingcapability data defining processing capabilities of each of the multipleUAVs. A set of UAVs may be selected based on the processing capabilitiesof each of the UAVs.

FIG. 11 illustrates a simplified flow diagram of an exemplary process1100 of enabling the handoff of tool systems between UAVs, in accordancewith some embodiments. In step 1102, a first UAV carrying a tool systemconfigured to perform a first function is identified. In some instances,the first UAV is identified through the central control system. In otherinstances, the first UAV is identified through a second UAV controlcircuit of a second UAV of multiple different UAVs of a task system 100.In step 1104, a notification is communicated to the first UAV directingthe first UAV to transfer the tool system to the second UAV. In step1106, a propulsion system of the second UAV is directed to control thesecond UAV to position the second UAV and couple the second UAV with thetool system transferred from the second UAV. In some instances, thefirst UAV is directed to disengage from the tool system and leave thetool system on the ground, in a mounting station, or other location. Thesecond UAV can proceed to the location of the tool system and couplewith and secure the tool system with the second UAV. In other instances,the first and second UAVs can communicate and coordinate the exchange ofthe tool system while both UAVs are in flight (e.g., while hoovering).In some applications, a first UAV can be directed to release a toolsystem at a location where a task is to be performed using the toolsystem.

Some embodiments in directing a UVA to transfer a tool system direct asecond UAV to hover at a defined location (e.g., GPS coordinates,mapping coordinates, etc.) and altitude, and direct a first UAV tocontrol its propulsion system to position the first UAV adjacent thesecond UAV and cause a coupling of the first UAV with the tool systemwhile the first UAV and the second UAV are in flight. The direction ofthe transfer of a tool system may include identifying a task beingperformed by a first UAV using a tool system is to continue to beperformed. A second UAV can be directed to control its propulsion systemto couple with the tool system and continue implementing the task usingthe tool system. This can allow the task to continue, such as when thefirst UAV is running out of power. In some instances, a power level of afirst UAV can be identified as being less than a threshold power level.A notification can be communicated to the first UAV directing the firstUAV to transfer the tool system based on the power level of the firstUAV being less than the threshold power level. Similarly, someembodiments confirm a power level of a tool system is greater than atool system power level threshold prior to causing a notification to becommunicated to a UAV directing the UAV to transfer the tool system.Further, some embodiments accessing a tool system database storing toolsystem parameter data associated with each of multiple tool systemsdefining functional capabilities and current location of each of themultiple tool systems, and can identify a tool system has afunctionality to be used to perform a task and further identify that thetool system is within a threshold distance of a UAV to be transferred tothe tool system, and/or within a threshold distance of a geographic areawhere a task is to be performed using the tool system. Some embodimentsidentify that a first UAV is predicted to complete a task beingperformed using the tool system within a threshold period of time priorto directing the transfer. This can ensure that a subsequent UAV to betransferred to tool system can perform a subsequent task or continue thetask within a desired time frame.

Further, some embodiments evaluate power levels of UAVs and/or toolsystem in selecting one or more UAVs and/or one or more tool systems tobe used in performing one or more tasks. The central control systemand/or a UAV control circuit can access power level data correspondingto each of the multiple UAVs and/or multiple tool systems. The centralcontrol system and/or UAV control circuit can evaluate the accessedpower level data, and select a second UAV of multiple UAVs and/or a toolsystem based at least in part on a power level of the second UAVrelative to a threshold power level. In some instances, the thresholdpower level corresponds to a first task to be performed, a predictedpower usage of a tool system to be temporarily cooperated with thesecond UAV and to be used in performing the first task, a safety marginpower level of a UAV, other such factors, or combination of two or moreof such factors.

FIG. 12 illustrates a simplified flow diagram of an exemplary process1200 of balancing power while managing UAVs in the performance of tasks,in accordance with some embodiments. In step 1202, power level data isaccessed by a first UAV control circuit of a first UAV of the multipleUAVs. The power level data can correspond to each of the multiple UAVs,and typically a current remaining power level data. In step 1204, theaccessed power level data is evaluated, typically relative to one ormore tasks to be performed. In step 1206, at least a second UAV isselected from the multiple UAVs based at least in part on a power levelof the second UAV relative to a threshold power level corresponding to afirst task to be performed and a predicted power usage of a first toolsystem to be temporarily cooperated with the second UAV and to be usedin performing the first task.

Some embodiments access a task predicted power usage database toidentify a predicted amount of power to be utilized by each of at leasttwo or more of the multiple UAVs to perform the task. Further, a powerlevel database may be accessed that maintain power level data of each ofthe multiple UAVs. The evaluation of power level data can includeevaluating the power level data indicating a current power level of eachof the two or more of the multiple UAVs relative to the predicted amountof power to be utilized. For example, a predicted amount of power can bedetermined that the second UAV is predicted to utilize to carry thefirst tool system to perform the first task. The prediction of theamount of power the second UAV is predicted to utilize can includeidentifying a predicted distance of travel by the second UAV inperforming the first task.

Further, some embodiments access predicted power usage by two or more ofmultiple tool systems to perform the first task, and select the firsttool system of the multiple tool systems based at least in part on apower level of the first tool system relative to a tool system thresholdpower level corresponding to the first task to be performed and apredicted power usage by the first tool system in performing the firsttask. Some embodiments direct a cooperative operation of each of themultiple UAVs in performing a set of different tasks and rotate the twoor more of the multiple UAVs between the different tasks to balancepower usage between the multiple UAVs. Power level usage can beevaluated relative to historic power level usage information inevaluating an efficiency of operation of the multiple UAVs. In someimplementations, the second UAV can be directed to cause power to bedrained from a power source of the first tool system and to be stored ina power source of the second UAV prior to the second UAV disengagingfrom the first tool system.

Some embodiments provide unmanned aerial task systems and methods ofmanaging tasks through unmanned vehicles. Some systems comprise:multiple unmanned aerial vehicles (UAV) each comprising: a UAV controlcircuit; a motor; and a propulsion system coupled with the motor andconfigured to enable the respective UAVs to move themselves; and whereina first UAV control circuit of a first UAV of the multiple UAVs isconfigured to identify a second UAV carrying a first tool systemconfigured to perform a first function, cause a notification to becommunicated to the second UAV directing the second UAV to transfer thefirst tool system to the first UAV, and direct a first propulsion systemof the first UAV to couple with the first tool system being transferredfrom the second UAV.

Some embodiments, provide methods of performing multiple different tasksthrough multiple unmanned aerial vehicles (UAV), comprising:identifying, through a first UAV control circuit of a first UAV of themultiple UAVs, a second UAV carrying a first tool system configured toperform a first function; causing a notification to be communicated tothe second UAV directing the second UAV to transfer the first toolsystem to the first UAV; and directing a first propulsion system of thefirst UAV to position the first UAV and couple the first UAV with thefirst tool system transferred from the second UAV.

Those skilled in the art will recognize that a wide variety of othermodifications, alterations, and combinations can also be made withrespect to the above described embodiments without departing from thescope of the invention, and that such modifications, alterations, andcombinations are to be viewed as being within the ambit of the inventiveconcept.

What is claimed is:
 1. An unmanned task system, comprising: multipleunmanned vehicles each comprising: an unmanned vehicle control circuitaccessing a tool system database; a motor; and a propulsion systemcoupled with the motor and configured to enable the respective unmannedvehicle to move itself; and wherein a first unmanned vehicle controlcircuit of a first unmanned vehicle of the multiple unmanned vehicles isconfigured to identify a second unmanned vehicle carrying a first toolsystem configured to perform a first function, cause a notification tobe communicated to the second unmanned vehicle directing the secondunmanned vehicle to transfer the first tool system to the first unmannedvehicle, cause the first unmanned vehicle to decouple from a second toolsystem configured to perform a second function that is different thanthe first function, and direct a first propulsion system of the firstunmanned vehicle to couple, using a universal coupler, with the firsttool system being transferred from the second unmanned vehicle enablingthe first unmanned vehicle to switch between the second tool system andthe first tool system and implement the first function provided throughthe first tool system.
 2. The system of claim 1, wherein the firstunmanned vehicle control circuit in directing the second unmannedvehicle to transfer the first tool system is configured to direct thesecond unmanned vehicle to release the first tool system at a locationwhere a task is to be performed using the first tool system.
 3. Thesystem of claim 1, wherein the first unmanned vehicle control circuit indirecting the second unmanned vehicle to transfer the first tool systemis configured to direct the second unmanned vehicle to a definedlocation; and the first unmanned vehicle control circuit in directingthe first propulsion system is configured to cause the first unmannedvehicle to position the first unmanned vehicle adjacent the secondunmanned vehicle and couple with the first tool system.
 4. The system ofclaim 3, wherein the first unmanned vehicle control circuit isconfigured to identify a task being performed by the second unmannedvehicle using the first tool system is to continue to be performed, anddirect the first propulsion system to couple with the first tool systemand continue implementing the task using the first tool system.
 5. Thesystem of claim 1, wherein the first unmanned vehicle control circuit isconfigured to identify a power level of the second unmanned vehicle isless than a threshold power level and to communicate the notification tothe second unmanned vehicle directing the second unmanned vehicle totransfer the first tool system based on the power level of the secondunmanned vehicle being less than the threshold power level.
 6. Thesystem of claim 1, wherein the first unmanned vehicle control circuit isconfigured to confirm a power level of the first tool system is greaterthan a tool system power level threshold prior to causing thenotification to be communicated to the second unmanned vehicle directingthe second unmanned vehicle to transfer the first tool system.
 7. Thesystem of claim 1, further comprising: the tool system database storingtool system parameter data associated with each of multiple tool systemsdefining functional capabilities and current location of each of themultiple tool systems, wherein the first unmanned vehicle controlcircuit is configured to access the tool system database, identify thefirst tool system has a functionality to be used to perform a task, andidentify that the first tool system is within a threshold distance ofthe first unmanned vehicle.
 8. The system of claim 1, wherein the firstunmanned vehicle control circuit, in identifying the second unmannedvehicle, is configured to identify the second unmanned vehicle ispredicted to complete a first task being performed using the first toolsystem within a threshold period of time.
 9. The system of claim 1,wherein the first unmanned vehicle control circuit is configured toidentify a task, which was being performed by the second unmannedvehicle using the first tool system, is to continue to be performed bythe first unmanned vehicle, and direct the first propulsion system andactivate the first tool system to continue implementing the task usingthe first tool system.
 10. The system of claim 9, further comprising:the universal coupler communicatively coupled with the unmanned vehiclecontrol circuit and a coupling system, wherein the universal coupler isconfigured to interchangeably couple with and decouple from the secondtool system and further interchangeably couple with and decouple withthe first tool system.
 11. The system of claim 9, further comprising:the tool system database storing tool system parameter data associatedwith each of multiple tool systems defining functional capabilities andcurrent location of each of the multiple tool systems, wherein the firstunmanned vehicle control circuit is configured to access the tool systemdatabase, identify the first tool system has a functionality to be usedto perform a task, and identify that the first tool system is within athreshold distance of the first unmanned vehicle.
 12. A method ofperforming tasks through unmanned vehicles each comprising a unmannedvehicle control circuit, comprising: identifying, through a firstunmanned vehicle control circuit of a first unmanned vehicle of themultiple unmanned vehicles, a second unmanned vehicle carrying a firsttool system configured to perform a first function; causing anotification to be communicated to the second unmanned vehicle directingthe second unmanned vehicle to transfer the first tool system to thefirst unmanned vehicle; causing the first unmanned vehicle to decouplefrom a second tool system configured to perform a second function thatis different than the first function; and directing a first propulsionsystem of the first unmanned vehicle to position the first unmannedvehicle relative to the first tool system aligning the first unmannedvehicle with the first tool system and to couple, using a universalcoupler, the first unmanned vehicle with the first tool systemtransferred from the second unmanned vehicle enabling the first unmannedvehicle to switch between the second tool system and the first toolsystem and to implement the first function provided through the firsttool system.
 13. The method of claim 12, wherein the directing thesecond unmanned vehicle to transfer the first tool system comprisesdirecting the second unmanned vehicle to release the first tool systemat a location where a task is to be performed using the first toolsystem.
 14. The method of claim 12, wherein the directing the secondunmanned vehicle to transfer the first tool system comprises directingthe second unmanned vehicle to a defined location; and wherein thedirecting the first propulsion system comprises positioning the firstunmanned vehicle adjacent the second unmanned vehicle and causing acoupling of the first unmanned vehicle with the first tool system. 15.The method of claim 14, further comprising: identifying a task beingperformed by the second unmanned vehicle using the first tool system isto continue to be performed, and directing the first propulsion systemto couple with the first tool system and continue implementing the taskusing the first tool system.
 16. The method of claim 12, furthercomprising: identifying a power level of the second unmanned vehicle isless than a threshold power level; and communicating the notification tothe second unmanned vehicle directing the second unmanned vehicle totransfer the first tool system based on the power level of the secondunmanned vehicle being less than the threshold power level.
 17. Themethod of claim 12, further comprising: confirming a power level of thefirst tool system is greater than a tool system power level thresholdprior to causing the notification to be communicated to the secondunmanned vehicle directing the second unmanned vehicle to transfer thefirst tool system.
 18. The method of claim 12, further comprising:accessing a tool system database storing tool system parameter dataassociated with each of multiple tool systems defining functionalcapabilities and current location of each of the multiple tool systems;identifying the first tool system has a functionality to be used toperform a task; and identifying that the first tool system is within athreshold distance of the first unmanned vehicle.
 19. The method ofclaim 12, wherein the identifying the second unmanned vehicle comprisesidentifying the second unmanned vehicle is predicted to complete a firsttask being performed using the first tool system within a thresholdperiod of time.